What was found
ROA - DURING 'CX-6' CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 2.75 INCH CRACK STR 24R STA 885 SKIN (FUSELAGE). STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ROA - DURING 'CX-6' CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 2.75 INCH CRACK STR 24R STA 885 SKIN (FUSELAGE). STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (X)